US4231703A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Variable guide vane arrangement and configuration for compressor of gas turbine devices
Assignee: MTU Aero Engines AG
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Filing: 1979-08-09
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Granted: 1980-11-04
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Expires: 1999-08-09
Abstract
Abstract Disclosed is a variable guide vane arrangement for use in a high-load compressor having at least one axial-flow stage in turbomachines including gas turbine engines, comprising a plurality of guide vanes positioned radially adjacent one another about a circumference in the axial flow stage of the compressor, each vane having a low-pressure and a high-pressure side during operation; a plurality of generally disk shaped turntable members, each of the vanes being secured at its outer end to one of the turntable members and each of the turntable members being rotatably mounted about the circumference, the diameter of each of the turntable members being greater than the spacing between adjacent guide vanes; and each of the turntable members being generally round and having a cut-out portion on the side adjacent to the low-pressure side of the guide vane secured thereto. The cut-out portion is formed by first, second and third arcs which merge together to form an edge surface adapted to closely abut the arcuate circumference of the next adjacent turntable member at all rotational settings of the guide vanes. The surface of each of the turntable members opposite to the side to which said guide vane is secured comprises a cone-shape having an apex angle equal to approximately 180°-360°/Z, wherein Z is the number of the guide vanes positioned about the circumference.
Inventors
- 👤 Wolfgang Weiler
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 02:11
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162; F04; F04D; F04D29/00; F04D29/40; F04D29/52; F04D29/54; F04D29/56; F04D29/563
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
177 words
A variable guide vane arrangement for use in a high-load compressor having at least one axial-flow stage in turbomachines including gas turbine engines, comprising: a plurality of guide vanes positioned radially adjacent one another about a circumference in the axial flow stage of the compressor, each vane having a low-pressure and a high-pressure side during operation; a plurality of generally disk shaped turntable members, each of said vanes being secured at its outer end to one of said turntable members and each of said turntable members being rotatably mounted about said circumference, the diameter of each of said turntable members being greater than the spacing between adjacent guide vanes; and each of said turntable members being generally round and having a cut-out portion on the side adjacent to the low-pressure side of said guide vane secured thereto, said cut-out portion being formed by first, second and third arcs which merge together to form an edge surface adapted to closely abut the arcuate circumference of the next adjacent turntable member at all rotational settings of said guide vanes.
Claim 2
Dependent Claim
177 words
A variable guide vane arrangement for use in a high-load compressor having at least one axial-flow stage in turbomachines including gas turbine engines, comprising: a plurality of guide vanes positioned radially adjacent one another about a circumference in the axial flow stage of the compressor, each vane having a low-pressure and a high-pressure side during operation; a plurality of generally disk shaped turntable members, each of said vanes being secured at its outer end to one of said turntable members and each of said turntable members being rotatably mounted about said circumference, the diameter of each of said turntable members being greater than the spacing between adjacent guide vanes; and each of said turntable members being generally round and having a cut-out portion on the side adjacent to the low-pressure side of said guide vane secured thereto, said cut-out portion being formed by first, second and third arcs which merge together to form an edge surface adapted to closely abut the arcuate circumference of the next adjacent turntable member at all rotational settings of said guide vanes.
Claim 3
Dependent Claim
45 words
A variable guide vane arrangement as defined by claim 1, wherein said first and third arcs are curved toward the low-pressure side of said vane and said second arc is positioned between said first and third arcs and is curved away from said low-pressure side.
Claim 4
Dependent Claim
33 words
A variable guide vane arrangement as defined by claim 2, wherein the radius of curvature of said first and third arcs comprises essentially the radius of the arcuate portion of said turntable members.
Claim 5
Dependent Claim
33 words
A variable guide vane arrangement as defined by claim 3, wherein the radius of curvature of said second arc comprises essentially the center-line distance between adjacent guide vanes minus said turntable member radius.
Claim 6
Dependent Claim
39 words
A variable guide vane arrangement as defined by claim 4, wherein the radius of curvature of said second arc equals the center-line distance between adjacent guide vanes minus said turntable member radius and the clearance between adjacent turntable members.
Claim 7
Dependent Claim
55 words
A variable guide vane arrangement as defined by claim 1, wherein the surface of each of said turntable members opposite to the side to which said guide vane is secured comprises a cone shape having an apex angle equal to approximately 180°-360°/Z, wherein Z is the number of said guide vanes positioned about said circumference.
Claim 8
Dependent Claim
51 words
A variable guide vane arrangement as defined by claim 6, wherein the outer casing of the compressor comprises adjacent recesses for receiving each of said turntable members and wherein the neighboring halves of each two adjacent recesses comprise surfaces opposite to the recess opening which lie on a common straight line.
Claim 9
Dependent Claim
53 words
A variable guide vane arrangement as defined by claim 1, wherein the shape of said first, second and third arcs is selected so that the clearance between said edge surface of each turntable member and said arcuate circumference of the adjacent turntable member remains constant for all rotational settings of said guide vanes.
Claim 10
Dependent Claim
34 words
A turbomachine comprising a compressor having at least one axial-flow stage and a variable guide vane arrangement positioned in said axial-flow stage, wherein said variable guide vane arrangement is as defined by claim 1.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-11-04 | 1984-05-05 | 1984-11-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-11-04 | 1988-05-05 | 1988-11-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-11-04 | 1992-05-05 | 1992-11-04 | $7700.00 | Window Closed / Lapsed |